View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 27561U 02054C 24357.52859033 .00000942 00000-0 21415-3 0 9999
2 27561 98.5116 195.8844 0044835 2.4211 357.7196 14.57810472171732
| Epoch (UTC): | 22 December 2024 12:41:10 |
| Eccentricity: | 0.0044835 |
| inclination: | 98.5116° |
| perigee height: | 668 km |
| apogee height: | 732 km |
| right ascension of ascending node: | 195.8844° |
| argument of perigee: | 2.4211° |
| revolutions per day: | 14.57810472 |
| mean anomaly at epoch: | 357.7196° |
| orbit number at epoch: | 17173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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